N548QS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NETJETS AVIATION, INC. (DXTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
REPEAT WRITE-UP, DURING PREFLIGHT AND AFTER BAGGAGE FIRE TEST WAS COMPLETED WE GOT RED BAGGAGE FIRE CAS AND A RED BAGGAGE FIRE PUSH BUTTON ILLUMINATED. APU SHUT DOWN. RAN CHECKLIST BUT DID NOT DISCHARGE FIRE BOTTLE. WENT TO VIZUALLY INSPECT BAGGAGE BAY, NO FIRE PRESENT BUT A VERY THIN HAZE OF SMOKE NOTED. LEFT BAGGAGE DOOR OPEN. AND RETURNED TO COCKPIT. SOME TIME AFTER MY RETURN THE RED BAGGAGE FIRE CAS WENT OUT AS DID THE RED BAGGAGE FIRE PUSH BUTTON. REPLACED BAGGAGE COMPARTMENT SMOKE DETECTOR IAW AMM 26-13-05. OPS CHECK GOOD.
ON CABIN PREP SYSTEMS TEST THE RED BAGGAGE FIRE TEST FAILS. THE RES CAS MESSAGE STAYS ILLUMINATED AND RED BAGGAGE FIRE BUTTON STAYS ILLUMINATED. UNABLE TO REAT OR TEST. CORRECTIVE ACTION; POWERED ON AIRCRAFT, COMPLETED MULTIPLE BAGGAGE COMPARTMENT SMOKE DETECTOR SYSTEM OPS CHECKS. ALL CHIMES, AURAL WARNINGS, CAS MESSAGES AND INDICATION LIGHTS CHECK GOOD AND EXTINGUISHED. REVIEWED CMC FOR FIRE PROTECTION FAULTS, NONE NOTED. PERFORMED ARES DOWNLOAD FOR 07/07 EVENTS AND SENT TO MANUFACTURER FOR EVALUATION. NOTIFIED MCC OF WORK PERFORMED, NOTED NO HISTORY NOTED AND NO FAULTS DURING MX. WORK COMPLETED IAW AMM CH 26-13-00 AND 31-33-00. OPS CHECK GOOD.
EMERGENCY LIGHTING: THE PAST FEW MORNINGS THE EMER LIGHTS DID NOT TEST WITH ARM OR COME ON IN THE ON POSITION DURING PREFLIGHT CHECKS. AFTER CHARGING FOR 15 MINUTES WITH THE APU ON THEY WORKED NORMALLY. CORRECTIVE ACTION; REPLACED ALL EMERGENCY BATTERY PACKS IAW CE 680A MM 33-50-06. OPS CHECK GOOD.
CABIN EMERG LIGHT: EMER LIGHTS COME ON FOR A SEC THEN GO OUT DURING PREFLIGHT TEST. CORRECTIVE ACTION: FOUND ALL 4 EMERGENCY LIGHT BATTERIES DISCHARGED. CHARGED BATTERIES AND PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK IAW CE 680A AMM 33-50-00. OPERATIONAL CHECK SATISFACTORY.
EMERG LIGHT SWITCH: SWITCH IS LOOSE AND SHORTING OUT. CORRECTIVE ACTION: GAINED ACCESS TO THE EMERG LIGHT SWITCH, PERFORMED A GVI NO DEFECTS NOTED, TIGHTEN THE SWITCH, CLOSED GAINED ACCFSS AND PERFORMED SEVERAL OPS CHECK SATISFACTORY IAW CE-680A AMM 33-50-00.
EMERGENCY LIGHTS ASSOCIATED WITH #3 EMER BATT PACK ARE INOPERATIVE. PERFORMED INSPECJION OF ALL EMERGENCY POWER SUPPLIES, WIRING, G SWITCHES AND RUSES WITH NO DEFECTS NOTED. PERFORMED BATTERY EXERCISE PROCEDURE WITH NO DEFECTS NOTED AND ALL EMERGENCY UGHTS WORKING AS REOUIRED.
MAIN DOOR: CABIN DOOR TOP STEP IS LOOSE AND HAS EXCESSIVE MOVEMENT. //SIGNOFF// VLSUALLY INSPECTED THE TOP STEP AND FOUND THE AFT HINGE BROKEN. REMOVED THE ASSEMBL Y FROM THE DOOR. DISCONNECTED THE TOP STEP ASSEMBLY FROM THE DOOR AND REPLACED THE THREE HINGES ON THE TOP STEP ASSEMBLY. RECONNECTED THE TOP IASSEMBL Y TO THE DOOR. REINSTALLED THE STEP ASSEMBLY ONTO THE DOOR. PERFORMED OPERATIONAL CHECK OF THE PROXIMITY SIGN AND ENTRY DOOR LIGHTS, OPS CHECK GOOD WORK PERFORMED IAW CE680A IMM 25-20-09.
WHILE EXTENDING THE SPEEDBRAKES IN FLIGHT WITH AUTOPILOT ON, WE EXPERIENCED THE LEFT WING DIP. THE AUTOPILOT MADE CORRECTIONS TO THE RIGHT WITH AILERONS. ALSO WHILE USING THE SPEEDBRAKE HANDLE, IT FELT SPONGY. IT FELT SMOOTH BUT AS IT GOT CLOSER TO THE DETENT FOR FULLY EXTENDED POSITION IT FELT LIKE IT WANT TO MOVE FORWARD TO THE STOWED POSITION. PERFORMED SPOILER POWER CONTROL UNIT PCU BUNGEE RIGGING AND FOUND THE RH #7 SPEEDBRAKE PANEL PCU BUNJEE OUT OF RIGGING.ADJUSTED THE BUNGEE ROD AS NECESSARY UNTIL RIGGING PIN WAS INSTALLED FREELY AND THE SPEEDBRAKE TRAVEL WAS WITHIN LIMITS. PERFORMED MULTIPLE SATISFACTORY OPERATIONAL CHECKS. ALL WORK PERFORMED IN REF WITH AMM 27-65-00.
THE MAIN DOOR HAND RAIL IS DETACHED, AND DOOR MOTOR DOES NOT ENGAGE. T/S FOUND DOOR HARDWARE MISSING AND- DOOR PIN THREADS DAMAGED REMOVED . DOOR RAIL PIN HINGE P/N 7411321-16 NSN INSTALLED NEW DOOR RAIL PIN HINGE P/N 7411321-16 NSN PERFOMRED SATISFACTORY OPERATIONAL CHECK NO DEFECTS NOTED IAW CE-680A AMM CHAPTER 52-10-40
AFTER TAKEOFF THE AIRCRAFT WOULD NOT PRESSURIZE. CABIN ALTITUDE WAS CLIMBING AT 1300 FPM REACHED APPROX 9500 FT CABIN ALTITUDE WHEN AT FL 180. COULD NOT CONTROL THE CABIN ALTITUDE IN EITHER AUTO OR MANUAL. COMPLIED WITH QRH PROCEDURES AND RETURNED FOR LANDING. INSPECTED OUTFLOW VALVE, FOUND INSULATION DEBRIS WRAPPED AROUND THE VALVE, BLOCKING THE AIRFLOW PATH AND PREVENTING THE VALVE FROM CLOSING. REMOVED INSULATION, RESTORED ACCESS. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED IN REFERENCE TO AMM 21-30-00.
RH ENGINE GEARBOX AFT COVER CORRODED IN MULTIPLE LOCATIONS.
LH HORIZONTAL STAB WEDGE PANEL UPPER AND LOWER NUTPLATE STRIP PN: 6932035-31 CORRODED.
R/H HORIZONTAL STABILIZER UPPER SKIN CORRODED AT NUTPLATE SPLICE STRIP P/N: 6932035-31.
L/H AND R/H APU UPPER BONDED SKIN ASSEMBLIES EXHIBIT CORROSION NEAR DEBRIS SHIELD. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ31884M1 REV. A DATED: 15OCT2021.
REPAIR OF RH MLG SIDE BRACE CHAFE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ30518M1 DATED: 06/29/2021, 680A-0105 (N548QS) RIGHT MAIN LANDING SIDE BRACE ACTUATOR INBOARD FITTING CHAFE DAMAGE.
NLG WHEEL WELL WEB AND UPPER MID FRAME CRACKED. TEXTRON AVIATION STANDARD REPAIR SR-680A ATA-25890 DATED: 6/1/2020, CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME WEB, AND DOUBLERS FS 75 WITH FAA FORM 8100-9 DATED: 6/1/2020.
PARK BRAKE ON AMBER CAS: IN FLIGHT, AFTER LANDING GEAR WAS EXTENDED, THE AMBER PARK BRAKE ON CAS ILLUMINATED. RAN QRH, AND YES, PARKING BRAKE HANDLE WAS STOWED. LANDED NORMALLY. PARKING BRAKE FUNCTIONS, EXCEPT WHEN YOU PRESS HANDLE DOWN, PARK BRAKE LOW PRESS CAS DISPLAYS.// SIGN OFF // REMOVED AND REPLACED PARKING BRAKE SWITCH WITH A NEW CUSTOMER SUPPLIED SWITCH WITH REF TO CE680A MM CHPT 32-44-15. OPERATIONAL CHECKS SATISFACTORY.
DURING ROTATION NR 2 ENG FIRE LIGHT ILLUMINATED WITH MASTER WARNING LIGHT & FIRE BELL. DURING EMERGENCY PROCEDURE FIRE LIGHT WENT OUT WHEN HANDLE WAS PULLED. FIRE BOTTLE WAS NOT DEPLOYED. ITEM IS UNDER INVESTIGATION.
WHEN APPLYING THE BRAKES FROM THE LT SEAT, THE FIRST APPLICATION RESULTS IN ALMOST NO BRAKING ACTION. THE PEDALS GO TO THE STOPS WITH VERY LITTLE RESULTS. BREAKING ACTION RETURNS TO NORMAL AFTER THE PEDALS ARE RELEASED AND RE-APPLIED. ITEM IS UNDER INVESTIGATION.
ON LANDING WHILE PULLING BACK ON THE THRUST REVERSER LEVERS, NR 1 ENGINE WENT TO SHUTDOWN AND NR 1 ENGINE FIRE LIGHT ILLUMINATED. PULLED NR 1 ENGINE FIRE BOTTLE, AIRCRAFT ARRIVED AT GATE WITHOUT FURTHER INCIDENTS. ITEM IS UNDER INVESTIGATION.
HOSE CLAMP HOLDING CUSTOM MADE AIRBOX TO PILOTS SIDE PANEL WAS POSITIONED SO THAT WORM SCREW OF CLAMP FOR SCREWDRIVER SLOT END WAS CUTTING INTO WIRES ON TERMINAL BLOCK MOUNTED BELOW BOX CAUSING FAILURE OF AUTOPILOT TRIM SYSTEM. THIS CONDITION EXISTED ON PILOTS AND COPILOTS SIDE PANELS. THE REPAIR WAS TO POSITION HOSE CLAMP WORM SCREW AT TOP OF AIRBOX AND COVERING WIRE TERMINAL BLOCK WITH PROTECTIVE TEFLON SHEET. DAMAGED WIRES REPAIRED AS REQUIRED.